Mathieu Lorteau

The Aircraft Noise Simulation Working Group (ANSWr) - V-2 Aircraft Results

Russell H. Thomas, Laurent Sanders, Lothar Bertsch, 2019 .

Numerical study, with experimental validation, of fan noise installation effects in Over-Wing Nacelle configuration using the Immersed Boundary Method

Stanislav L. Denisov, Victor F. Kopiev, Ludovic Wiart, 2019 .

Comparative Assessment of Aircraft System Noise Simulation Tools

Laurent Sanders, Ingrid LeGriffon, Lothar Bertsch, 2021, Journal of Aircraft.

Turbulent jet simulation using high-order DG methods for aeroacoustics analysis

Vincent Couaillier, Mathieu Lorteau, V. Couaillier, 2017, 1705.08723.

Analysis of noise radiation mechanisms in hot subsonic jet from a validated large eddy simulation solution

Francois Vuillot, Mathieu Lorteau, Franck Cléro, 2015 .

Large Eddy Simulation of Jet Noise from Unstructured Grids with Turbulent Nozzle Boundary Layer

Francois Vuillot, Mathieu Lorteau, Franck Cléro, 2016 .